|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
up to 1,500 ° F
|
|
gptkbp:bypass_ratio
|
5.5:1
|
|
gptkbp:compressor_type
|
gptkb:10
axial
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
3.0 ft
2.54 m
|
|
gptkbp:emissions_standard
|
ICAO Chapter 3
|
|
gptkbp:engine
|
advanced aerodynamics
modular design
advanced materials
computer-aided design
advanced cooling techniques
noise reduction technology
digital engine control
high-efficiency fan blades
variable area nozzle
high-efficiency combustor
low-emission combustor
high-pressure ratio
|
|
gptkbp:engine_configuration
|
twin-engine
pylon-mounted
|
|
gptkbp:engine_power
|
20,000 hours
|
|
gptkbp:engine_type
|
dual-spool
|
|
gptkbp:fan_blades
|
gptkb:22
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
3.81 m
0.91 m
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-50 C5
|
|
gptkbp:is_tested_for
|
static test
flight test
|
|
gptkbp:length
|
12.5 ft
|
|
gptkbp:maintenance
|
4,000 hours
overhaul every 10,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:notable_users
|
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:propulsion
|
50,000 lbf
12.5:1
|
|
gptkbp:service_entry
|
gptkb:1971
|
|
gptkbp:successor
|
CF6-80 C2
|
|
gptkbp:turbine_blades
|
gptkb:10
|
|
gptkbp:turbine_type
|
2
high bypass turbofan
|
|
gptkbp:weight
|
4,000 lb
|
|
gptkbp:bfsParent
|
gptkb:CF6-50_C
|
|
gptkbp:bfsLayer
|
7
|